Q1568697: Difference between revisions
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Q1568697
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{{Page|Sea Dragon|Classes|1962 concept for a reusable, sea-launched rocket}} | {{Page|Sea Dragon|Classes|1962 concept for a reusable, sea-launched rocket|}} | ||
Latest revision as of 13:17, 17 February 2025
The Sea Dragon was a 1962 conceptualized design study for a two-stage sea-launched orbital super heavy-lift launch vehicle. The project was led by Robert Truax while working at Aerojet, one of a number of designs he created that were to be launched by floating the rocket in the ocean. Although there was some interest at both NASA and Todd Shipyards, the project was not implemented.
1962
Wikimedia, Wikidata
length 150 metre, payload mass 550 tonne, diameter 23 metre,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, super heavy-lift launch vehicle, 1962, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
Sea-Dragon
A computer generated image of the Sea Dragon (rocket)A computer generated image of the Sea Dragon (rocket)| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Sea-Dragon | Commons | ||
| commons | image | A computer generated image of the Sea Dragon (rocket) | Commons | ||
| commons | image | A computer generated image of the Sea Dragon (rocket) | Commons | ||
